Optical performance of thin film, inflatable, solar concentrators for illuminating PV arrays
Michael R. J. Holmes
Abstract
Michael R. J. Holmes
Abstract
Inflatable technology for antennas and solar concentrators is rapidly maturing. Large inflatable paraboloids, developed for space propulsion systems and antennas are now available for ground test of power systems. Inflatable structures can potentially reduce spacecraft weight and decrease the volume required by a power system. Reflective surfaces do not require much mass so that inflatable antennas or concentrators can be very lightweight. Inflatables can also be packaged more compactly than rigid structures thereby reducing volume constraints in a faring. Therefore, we believe that space power applications could benefit from this technology. This paper includes a basic analysis of a candidate power system using an optical ray-trace code. By using a large area concentrator, it is hoped that the paraboloid concentrators for solar-thermal propulsion. This analysis will show if a uniform distribution of light can be concentrated on a photovoltaic array so that useful power might be generated. In the future, other technical challenges must be addressed. In particular, heat rejection will be a problem since then must be accomplished from the smaller area of the photovoltaic array as opposed to the area of the concentrator.
OpenAlex reports 2 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
Inflatable technology for antennas and solar concentrators is rapidly maturing. Large inflatable paraboloids, developed for space propulsion systems and antennas are now available for ground test of power systems. Inflatable structures can potentially reduce spacecraft weight and decrease the volume required by a power system. Reflective surfaces do not require much mass so that inflatable antennas or concentrators can be very lightweight. Inflatables can also be packaged more compactly than rigid structures thereby reducing volume constraints in a faring. Therefore, we believe that space power applications could benefit from this technology. This paper includes a basic analysis of a candidate power system using an optical ray-trace code. By using a large area concentrator, it is hoped that the paraboloid concentrators for solar-thermal propulsion. This analysis will show if a uniform distribution of light can be concentrated on a photovoltaic array so that useful power might be generated. In the future, other technical challenges must be addressed. In particular, heat rejection will be a problem since then must be accomplished from the smaller area of the photovoltaic array as opposed to the area of the concentrator.
Key concepts: Inflatable, Photovoltaic system, Paraboloid, Spacecraft, Aerospace engineering, Concentrator, Solar mirror, Solar cable